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Cessna 337 skymaster manual
Cessna 337 skymaster manual





This is due to the aircraft's engine configuration. The Cessna 337 will not yaw into the dead engine if one engine fails. Reims in France also built several models of the aircraft. Cessna produced civil and military variants of the 337. A turbocharged variant (T337) was introduced in 1966 and a pressurized variant (P337G) was introduced in 1973. The 337 had retractable landing gear and a dorsal air scoop for the rear engine. The 337 Super Skymaster was introduced in 1965. Combined tractor and pusher engines produce centerline thrust. Mounted between and connecting the two booms, the horizontal stabilizer is aft of the pusher propeller. With the rear engine between them, twin booms extend aft of the wings to the vertical stabilizers. Variant Cessna models include the 327 Baby Skymaster, 336 Skymaster, Model 337 Super Skymaster, 337A Super Skymaster, 337B Super Skymaster, T337 Turbo Super Skymaster, 337C Super Skymaster, 337D Super Skymaster, 337E Super Skymaster, 337F Super Skymaster, 337G Super Skymaster, P337 Super Skymaster, 337H Super Skymaster, P337H Pressurized Skymaster, 337M, O-2A, O-2B, O-2TT, Summit Sentry O2-337, Lynx, and T337G. 2993 aircraft were produced from 1963 to 1982. The Skymaster's engines are mounted in the nose and rear of its pod-style fuselage. The maximum speed is 174 knots (200 mph, 320 km/h) and the rate of climb is 1200 ft/min (6.1 m/s). The empty weight is 2655 lb (1204 kg) and the maximum takeoff weight is 4400 lb (2000 kg). The Cessna 337 has the capacity for one crew member and five passengers. Built in a push-pull configuration, the Cessna Skymaster is a United States twin-engined civil utility aircraft.







Cessna 337 skymaster manual